飞行试验用低成本数据采集装置

Q4 Engineering Fatigue of Aircraft Structures Pub Date : 2019-12-01 DOI:10.2478/fas-2019-0012

Błażej Morawski, D. Głowacki, Anna Głowacka

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引用次数: 0

摘要

摘要:本文介绍了一种全尺寸飞机和无人机飞行试验数据记录仪的设计。该记录仪是基于Arduino微处理器平台和LabVIEW开发环境构建的。数据记录仪将主要用于直升机飞行试验。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Low-Cost Data Acquisition Unit for Flight Tests

Abstract The purpose of this paper is to present the design of a data recorder for flight tests of a full-scale aircraft and an UAV. The recorder is built based on the Arduino microprocessor platform and LabVIEW development environment. The data recorder will be used mainly for helicopter flight tests.

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来源期刊

Fatigue of Aircraft Structures Engineering-Safety, Risk, Reliability and Quality

CiteScore

0.40

自引率

0.00%

发文量

期刊介绍： The publication focuses on problems of aeronautical fatigue and structural integrity. The preferred topics include: full-scale fatigue testing of aircraft and aircraft structural components, fatigue of materials and structures, advanced materials and innovative structural concepts, damage tolerant design of aircraft structure, life extension and management of ageing fleets, structural health monitoring and loads, fatigue crack growth and life prediction methods, NDT inspections, airworthiness considerations.